WO2014040462A1 - 一种登机桥接机口装置和具有其的登机桥及其接机方法 - Google Patents

一种登机桥接机口装置和具有其的登机桥及其接机方法 Download PDF

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Publication number
WO2014040462A1
WO2014040462A1 PCT/CN2013/081213 CN2013081213W WO2014040462A1 WO 2014040462 A1 WO2014040462 A1 WO 2014040462A1 CN 2013081213 W CN2013081213 W CN 2013081213W WO 2014040462 A1 WO2014040462 A1 WO 2014040462A1
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WO
WIPO (PCT)
Prior art keywords
boarding bridge
flap
main body
movable floor
pick
Prior art date
Application number
PCT/CN2013/081213
Other languages
English (en)
French (fr)
Inventor
向卫
石磊
康达
张肇红
Original Assignee
深圳中集天达空港设备有限公司
中国国际海运集装箱(集团)股份有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 深圳中集天达空港设备有限公司, 中国国际海运集装箱(集团)股份有限公司 filed Critical 深圳中集天达空港设备有限公司
Priority to EP13837069.7A priority Critical patent/EP2896569A4/en
Priority to BR112015005805A priority patent/BR112015005805A2/pt
Priority to CA2885108A priority patent/CA2885108C/en
Priority to SG11201502072UA priority patent/SG11201502072UA/en
Priority to AU2013314929A priority patent/AU2013314929A1/en
Priority to RU2015111985A priority patent/RU2015111985A/ru
Priority to US14/428,824 priority patent/US9434482B2/en
Publication of WO2014040462A1 publication Critical patent/WO2014040462A1/zh

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/30—Ground or aircraft-carrier-deck installations for embarking or disembarking passengers
    • B64F1/305—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable
    • B64F1/3055—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable with hinged head interface between aircraft and passenger bridge
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/30—Ground or aircraft-carrier-deck installations for embarking or disembarking passengers
    • B64F1/305—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable

Definitions

  • the present invention relates to a boarding bridge, and more particularly to a boarding bridge port device and a boarding bridge having the same and a method of picking up the same.
  • the boarding bridge provides safe and comfortable walking space for passengers entering and leaving the airport and has been widely used at airports.
  • most of the boarding bridges can be used for docking services for left and right door-opening aircraft.
  • the existing regional aircrafts are designed to be opened in the form of a handrail with a gangway, that is, an aircraft that opens the door downwards.
  • the existing boarding bridges designed for left and right door-opening aircraft will interfere with the operation of the aircraft door that opens the door. It is unable to serve such aircraft and cannot meet the feeder line. Docking requirements between the aircraft and the boarding bridge. Invention disclosure
  • the technical problem to be solved by the present invention is to provide a boarding bridge device and a boarding bridge having the same and a method of picking up the same, which can simultaneously serve an aircraft that opens and closes the door and an airplane that opens the door.
  • the present invention provides a boarding bridge device, which is installed at the front end of a docking platform of a boarding bridge, and includes:
  • a movable floor main body a rear end of the movable floor main body is connected to a front end of the docking platform, and a front end of the movable floor main body is provided with a notch, and the notch is adapted to receive a door of an aircraft to be turned down or turned up;
  • the pushing device comprising: a mounting bracket, fixedly connected a bottom of the movable floor body; a pusher, one end of the pusher is coupled to the mounting bracket, and the other end of the pusher is coupled to the bottom of the flap.
  • the boarding bridge device further includes a semi-automatic locking mechanism, comprising: a bolt mounting structure disposed at the bottom of the flap, the bolt mounting knot a locking bolt is mounted on the locking tongue, and the first spring is disposed on the locking tongue; the first locking hole mounting structure is correspondingly disposed corresponding to the position of the locking tongue mounting structure when the flap is in the first position
  • the first locking hole mounting structure has a first locking hole for receiving the locking tongue, and the pulling out of the locking tongue is manually operated. The resetting of the bolt is automatically reset by the spring, and the flap is lockedly coupled to the raised floor body by the lock tongue being received in the first lock hole when in the first position.
  • the semi-automatic latch mechanism further includes: a second keyhole mounting structure corresponding to a position of the bolt mounting structure when the flap is in the second position Provided in a second mounting position of the bottom of the raised floor main body, the second keyhole mounting structure has a second locking hole for receiving the locking tongue; wherein the flap is in the second In position, the lock tongue is locked in the second lock hole to be lockedly connected to the movable floor main body.
  • the semi-automatic locking mechanism further comprises: an inductive switch, wherein the first locking hole and the second locking hole are disposed on the first locking hole mounting structure and the The second keyhole mounting structure; the backing plate is correspondingly disposed in the first locking hole and the second locking hole.
  • the semi-automatic latch mechanism further comprises: a blocking piece movably mounted on the movable floor main body corresponding to the first locking hole and the second locking hole.
  • the semi-automatic latch mechanism is symmetrically disposed on the left and right sides of the bottom of the front end of the flap.
  • At least one side surface of the left and right sides of the flap is further provided with a trapezoidal guiding block, and the two trapezoidal inclined surfaces of the trapezoidal guiding block are arranged up and down.
  • a pressure sensing device is disposed on a bottom of the raised floor main body corresponding to at least one of left and right sides of the flap, each of the pressure sensing
  • the device includes: a lever mechanism including a bending rod, a straight rod, a wedge and a second spring, wherein one end of the curved rod is hinged at a bottom of the raised floor body, and the other end is hinged with the straight rod; One end of the two springs is connected to the bottom of the raised floor body, the other end is connected to the curved rod; the wedge is fixedly connected to the one end of the curved rod; the sliding mechanism includes a sliding slot and sliding Block, the chute is fixedly mounted on the bottom of the raised floor main body, the slider is fixedly mounted on the straight rod; and a pressure sensor is fixedly mounted on the straight rod.
  • the bending rod comprises a first portion, a second portion and a third portion, wherein the third portion is a bent portion, and the two ends of the third portion are respectively Bend a first hinge point hinged by the rod to the bottom of the raised floor body and a second hinge point hinged by the curved rod and the straight rod, the first portion and the third portion being connected to the first hinge point
  • the wedge is fixedly coupled to the first portion, and the second portion is coupled between the first portion and the third portion.
  • the boarding bridge device of the above wherein the boarding bridge device further comprises a transportable movable ferry board, wherein the transportable movable board is used to be in the second The gap is closed when in position.
  • the present invention further provides a boarding bridge, the boarding bridge including a pick-up platform, wherein the boarding bridge further includes the above-mentioned front end connected to the front end of the pick-up platform The boarding bridge device described.
  • the present invention also provides a pick-up method using the boarding bridge as described above, which includes:
  • the flap of the boarding bridge device When serving the aircraft opening and closing the door, the flap of the boarding bridge device is turned to the first position, so that the flap closes the gap on the movable floor main body of the boarding bridge device to form a complete And picking up the boarding bridge, and the boarding bridge device is overlapped with the door of the left and right door to form a pick-up channel for pick-up.
  • the flap of the docking device When the aircraft is opened under the service, the flap of the docking device is first turned down to the second position to expose the gap on the movable floor main body of the boarding bridge device, and then the exposed The notch is aligned with the door of the aircraft that opens the door, and the boarding bridge is operated such that the notch completely accommodates the door, and then the end of the movable movable plate is lapped at the boarding bridge The gap is closed on the machine mouth device, and the other end is overlapped on the floor surface of the aircraft to form a pick-up channel for pick-up.
  • FIG. 1 is a side view of a boarding bridge device according to an embodiment of the present invention, wherein Two different states when the flap is in the first position A and the second position A' is reversed, and the boarding bridge device is in the unconnected state;
  • FIG. 2 is a top plan view of the boarding bridge device shown in FIG. 1 (the flap is in the first position A);
  • Figure 5 is a cross-sectional view taken along line 13-13 of Figure 3;
  • Figure 6 is a front elevational view of the boarding bridge device of Figure 2;
  • Figure 7 is an enlarged schematic view showing the structure of the portion C in Figure 6;
  • Figure 8 is a cross-sectional view taken along line 14-14 of Figure 6;
  • Figure 9 is a cross-sectional view taken along line 15-15 of Figure 2, showing a side view of the flap when in the first position A;
  • Figure 10 is a side elevational view of the flap of Figure 9 in a second position A';
  • Figure 11 is a schematic view of the aircraft door when it is opened
  • Figure 12 is a side elevational view of a boarding bridge port apparatus in accordance with an embodiment of the present invention, wherein the boarding bridge interface unit is in an on-off state.
  • FIG. 1 shows a boarding bridge 100 according to an embodiment of the present invention, which includes a docking platform 10 and a boarding bridge port device 20.
  • the boarding bridge device 20 is installed at the front end of the docking platform 10 for docking with the aircraft door.
  • the boarding bridge apparatus 20 of the present invention includes a raised floor body 30 and a flap 40 and a pushing device 50.
  • the left and right sides of the rear end B of the raised floor main body 30 are provided with ferry plates 321 and 322.
  • the ferry plates 321 and 322 have a triangular structure for use with the docking platform 10 (in FIG. 2 Not shown) connected.
  • the front end F of the raised floor main body 30 is provided with a notch 31 (the notch 31 in Fig. 2 is blocked by the flap 40), and the notch 31 can be adapted to accommodate a door of an aircraft to be turned down or up.
  • the notch 31 is square.
  • the flap 40 is disposed corresponding to the notch 31 and is movably connected to the raised floor main body 30, for example, hinged to the movable floor main body 30 on the rear end side of the notch 31 by a flap hinge 41, thereby
  • the flap 40 can be flipped at an angle relative to the raised floor main body 30 along the flap hinge 41, as shown in FIG.
  • the state in which the notch 31 is closed when the plate 40 is in the first position A (indicated by a chain double-dashed line) and the state in which the flap 40 is reversed toward the second position A'.
  • a schematic view of the side of the flap 40 flipped to the second position A' is shown in Fig. 10.
  • the first position A is a position when the flap 40 is level with the raised floor main body 30, that is, the working position of the docking station device 20 serving the aircraft left and right to open the door; the second position A' is the flap 40
  • the position between the angle with the raised floor main body 30 is greater than 90° (as determined as needed), i.e., the docking station device 20 serves the working position when the aircraft is turned down.
  • the pushing device 50 is used to push the flap 40 to reverse.
  • the pushing device 50 comprises a mounting bracket 51 and a pusher 52, wherein the mounting bracket 51 is fixedly connected to the bottom of the raised floor main body 30, and one end of the pusher 52 is connected (optionally connected by a pin) at the installation On the bracket 51, the other end of the pusher 52 is connected (optionally connected by a pin) at the bottom of the flap 40.
  • the pusher 52 is disposed substantially along the centerline of the flap 40, and the other end thereof is coupled to a central position of the bottom of the flap 40.
  • the front end of the raised floor main body 30 (the front end other than the notch 31) is provided with detachable leading edges 331, 332, 333, and a detachable leading edge is also provided on the front end of the flap 40. 43, to enhance the protection of the aircraft during the docking process.
  • the outer edges of the mounted leading edges 331, 332, 333 and 43 remain substantially flush.
  • the detachable leading edges 331, 332, 333 and the detachable leading edge 43 are connectable to the raised floor body 30 and the flap 40 by bolts and nuts (as shown in Figures 9, 10), currently When the edge damage needs to be replaced or repaired, the disassembly process is convenient.
  • the boarding bridge apparatus 20 of the present invention may also include a semi-automatic latch mechanism 37.
  • the semi-automatic latch mechanism 37 is symmetrically disposed on the left and right sides of the bottom end of the front end of the flap 40.
  • the semi-automatic latch mechanism 37 includes a first keyhole mounting structure 371 and a bolt mounting structure 372 that are correspondingly mounted.
  • the bolt mounting structure 372 is disposed at the bottom of the flap 40 and is provided with a locking tongue 374.
  • the locking tongue 374 is provided with a first spring 376.
  • the first keyhole mounting structure 371 is corresponding to the position of the bolt mounting structure 372 when the flap 40 is in the first position A, and is correspondingly disposed at the first mounting position of the bottom of the raised floor main body 30. For example, it is disposed on the bottom of the front end of the raised floor main body 30, and the first keyhole mounting structure 371 has a first locking hole 373 for receiving the locking tongue 374.
  • the present invention employs a semi-automatic latch mechanism 37, that is, the pullout of the bolt 374
  • the reset of the bolt 374 is automatically reset by the first spring 376.
  • the semi-automatic latch mechanism 37 can also lock the flap with other locking mechanisms.
  • the semi-automatic latch mechanism 37 can also be disposed only on the left or right side of the front end of the flap 40. These are not intended to limit the invention.
  • the semi-automatic latch mechanism 37 further includes: two second keyhole mounting structures 37 ⁇ disposed symmetrically to the left and right, corresponding to the lock when the flap 40 is in the second position A'
  • the position of the tongue mounting structure 372 corresponds to a second mounting position disposed at the bottom of the raised floor main body 30, and each of the second keyhole mounting structures 37a has a second locking hole for receiving the locking tongue 374. 373 '.
  • the flap 40 is in the first position A by the locking structure 37a composed of the first keyhole mounting structure 371 and the bolt mounting structure 372 and the raised floor.
  • the main body 30 is in a locking connection.
  • the locking tongue 374 is received in the first locking hole 373, and the flap 40 is substantially flush with the raised floor main body 30.
  • the flap 40 when the flap 40 is in the second position A', it is connected to the raised floor body by a locking structure 37a' composed of a second keyhole mounting structure 37" and a tongue mounting structure 372. 30, the locking connection is performed.
  • the locking tongue 374 is received in the second locking hole 373 ′, and when the flap 40 is in the second position A′, the aircraft door does not turn down. Interference with the flap 40.
  • an inductive switch 375 and a backing plate 377 are disposed on the first keyhole mounting structure 371.
  • the sensing switch 375 is disposed corresponding to the first locking hole 373 to detect whether the locking tongue 374 is reset to a predetermined position.
  • the pad 377 is correspondingly disposed in the first locking hole 373 for The locking tongue 374 is prevented from touching the damage sensing switch 375, and the distance from the sensing switch 375 after the locking tongue 374 is reset reaches a predetermined value.
  • an inductive switch and a pad can also be disposed on the second keyhole mounting structure 37A.
  • the structure, function and arrangement position are similar to those of the inductive switch 375 and the pad 377 shown in FIG.
  • the inductive switch on the second keyhole mounting structure 37A is disposed corresponding to the second locking hole 373', and the pad on the second keyhole mounting structure 37 is correspondingly disposed on the second locking hole 373 'inside.
  • the semi-automatic locking mechanism further includes four blocking pieces: correspondingly movable to the movable floor corresponding to the two first locking holes 373
  • the blocking pieces 38, 38' are connected to the movable floor main body through pins 381, 38 ,, and are respectively disposed at corresponding positions when the flaps are in the first position A and the second position A'. For manually pulling out the bolt 374, blocking the first locking hole 373 and the second locking hole 373 '.
  • upper limit members 391, 39 ⁇ and lower limit members 392, 392 ' are respectively disposed on the movable floor main body 30 at positions corresponding to the upper and lower sides of the baffles 38, 38', respectively.
  • the limit of the baffle 38, 38 'rotating up and down for example:
  • the baffle 38 blocks the first lock hole 373; after the button is manually operated, the flap 40 starts from the first A position A is turned over toward the second position A', and when the flap 40 is turned to the lowest position (i.e., turned to the position where the center of gravity of the flap 40 is lowest), and then continues to be turned up to a position close to the second lock hole 373',
  • the locking tongue 374 touches the pressing baffle 38' upwardly, so that the baffle 38' is rotated upwardly about the pin 38 ⁇ to the state when the upper limit member 39 is restrained, and the locking tongue 374 is received in the second locking hole. 373 ' and lock.
  • the baffle 38' When the task of turning the door opener is completed, the baffle 38' is manually rotated from the second lock hole 373', and the baffle 38' is rotated downwardly about the pin 38 ⁇ under the action of the heavy moment to the receiving position.
  • the baffle 38 rotates the baffle 38 upwardly about the pin 381 to a state when the upper limit member 391 is restrained, as shown by the solid line in FIG. 4, and the lock tongue 374 is accommodated therein.
  • the first lock hole 373 is locked.
  • trapezoidal guide blocks 36 are respectively disposed on the left and right side faces of the flap 40, which are fixed by screws, and are preferably made of nylon.
  • the two trapezoidal inclined faces 361, 362 of the trapezoidal guide block 36 are arranged up and down, and are guided during the turning of the flap 40 to the first position A and the second position A'.
  • the trapezoidal guide 36 also maintains a spacing between the flap 40 and the raised floor body 30 to prevent interference or friction between the two.
  • the trapezoidal guide block 36 may also be disposed only on the left or right side of the flap 40, which are not intended to limit the invention.
  • a pressure sensing device 60 is disposed on each of the left and right sides of the bottom of the raised floor main body 30 adjacent to the left and right sides of the flap 40.
  • each of the pressure sensing devices 60 includes a lever mechanism 61, a slide mechanism 62, and a pressure sensor 63.
  • the lever mechanism 61 includes a bending rod 611, a straight rod 612, a wedge 613, and a second spring 614.
  • One end of the curved rod 611 is hinged to the bottom of the raised floor main body 30 by a pin, and the other end is hinged with the straight rod 612 through a pin.
  • One end of the second spring 614 is coupled to the bottom of the raised floor main body 30, and the other end is coupled to the curved rod 611.
  • the curved rod 611 includes a first portion 6111, a second portion 6112, and a third portion 6113, wherein the third portion 6113 is a bent portion, and the two ends of the third portion 6113 are respectively a first hinge point 61a hinged with the bottom of the raised floor body 30 and a second hinge point 61b hinged by the curved rod 611 and the straight rod 612, the first portion 6111 and the third portion a portion 6113 is coupled to the first hinge point 61a, and the wedge 613 is fixedly coupled to the one end of the curved rod 611 by screws, specifically to the first portion 61 11
  • the second portion 6112 is coupled between the first portion 6111 and the third portion 6113.
  • the connection position 61c of the other end of the second spring 614 is close to the second hinge point 61b.
  • the sliding mechanism 62 includes a sliding slot 621 and a slider 622.
  • the chute 621 is fixedly mounted at the bottom of the raised floor main body 30, and the slider 622 is fixedly mounted on the straight rod 612.
  • the pressure sensor 63 is fixedly mounted on the straight rod 612.
  • the working process of the pressure sensing device 60 is described as follows: When the flap 40 is turned to a certain position close to the second position A', the flap 40 is pressed against the wedge 613 to push the curved rod 61 1 Rotating around the first hinge point 61a, thereby pushing the left and right pressure sensors 63 fixedly coupled with the straight rod 612 to slide out in a direction perpendicular to itself with the cooperation of the sliding mechanism 62 (in the process, the second spring 614 is stretched).
  • the function of the pressure sensor 63 is to prevent interference or collision between the two sides of the notch 31 and the aircraft door/suspension/suspended handrail during the pick-up process.
  • FIG. 9 it shows the state when the flap 40 is in the first position A. At this time, the flap 40 is flush with the raised floor main body 30, at this time corresponding to the two second locking holes 373, the position Two flaps 38 block the two second locking holes 373 '.
  • FIG. 10 shows the state in which the flap 40 is in the second position A', at which time the flap 40 is at a predetermined angle with the raised floor main body 30, corresponding to the position of the two first lock holes 373.
  • the two flaps 38 block the two first locking holes 373.
  • Figure 1 is a schematic view of the door of the aircraft that opens the door when it is opened. At this time, the door 91 of the aircraft 90 with the suspension handrail 911 is turned down to expose the door door 92.
  • FIG. 12 is a side elevational view of the boarding bridge device in the state of pick-up, in which the flap 40 is in the second position A', and the boarding bridge device 20 passes through it according to an embodiment of the present invention.
  • a notch 31 in the movable floor main body 30 accommodates the door 91 therein.
  • the boarding bridge device 20 of the present invention is further provided with a movable transporting plate (not shown) for closing the gap 31 when the flap 40 is in the second position A'.
  • a pick-up channel is formed and the passenger can get on and off the plane.
  • the flap 40 of the boarding bridge device 20 When servicing an aircraft that opens the door to the left and right, the flap 40 of the boarding bridge device 20 is turned to the first position A, so that the flap 40 closes the raised floor main body 30 of the boarding bridge device The notch 31, and the flap 40 is securely locked with the raised floor main body 30 by a semi-automatic latch mechanism 37 to form a complete pick-up passage, and then the boarding bridge is operated to make the boarding bridge port The device 20 is overlapped with the door of the left and right open door to form a pick-up channel for pick-up. At this time, the same as the ordinary pick-up port can serve the left and right open doors.
  • the operator can first pull out the lock tongue of the semi-automatic lock mechanism 37 under the pick-up platform 10 (the reason for manually pulling the lock tongue is to prevent the operator from misoperation, If a staff member or passenger is standing on the pick-up platform, the operator may endanger the life of the person if the flap is turned down. Therefore, the operator needs to manually pull the lock tongue. After the lock tongue is pulled out, the operator goes to board the plane. On the bridge, pressing the button causes the flap 40 to be turned over. When the flap 40 is turned to a position close to the second position A', the flap 40 is pressed against the wedge 613 of the lever mechanism 61 and will be mounted on the lever.
  • the pressure sensor 63 on the mechanism 61 slides out to the two sides of the notch 31 of the flap through the sliding mechanism 62 (after the pressure sensor is turned over, it can detect whether the aircraft door/gangway/overhanging handrail will touch when the machine is connected
  • the flap 40 continues to be turned to the second position A', the locking tongue of the semi-automatic locking mechanism 37 automatically springs into the corresponding locking hole and is locked; the operator closes the notch 31 of the flap 40 Pilot 91, operating the boarding bridge forward until the docking station device 20 contacts the fuselage, at which time the notch 31 completely accommodates the door 91; then the operator places one end of the transportable movable ferry board at the boarding bridge device 20
  • the gap 31 is closed and the other end is placed on the floor surface of the aircraft to form a pick-up passage, and the passenger can get on and off the plane.
  • the operator retracts the movable transfer board; the bridge is retracted until the door 91 is completely withdrawn from the gap 31; then, the lock tongue 374 of the locked semi-automatic lock mechanism 37 is pulled down to the pick-up platform. And pressing the button causes the flap 40 to be turned from the second position A' to the first position A. In the process, the flap 40 gradually no longer squeezes the lever mechanism 61, and the pressure sensor 63 is in the second spring 614.
  • the locking tongue of the semi-automatic locking mechanism 37 automatically springs into the corresponding locking hole and is locked, and the flap 40 is at the first position A, and the pick-up process is completed.
  • the aircraft that opens and closes the door and the plane that opens the door can be served at the same time, which can well meet the docking requirements between the regional aircraft and the boarding bridge.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Bridges Or Land Bridges (AREA)
  • Platform Screen Doors And Railroad Systems (AREA)
  • Elevator Door Apparatuses (AREA)
  • Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)

Abstract

一种登机桥接机口装置（20），包括：活动地板主体（30），活动地板主体的后端（B）与接机平台（10）的前端连接，活动地板主体的前端（F）上设置有一缺口（31），所述缺口适于容纳一飞机的机门下翻或上翻；翻板（40），对应于该缺口设置并与活动地板主体活动连接，且所述翻板相对于所述活动地板主体在一第一位置（A）与一第二位置（Α'）之间翻转，翻板在处于第一位置时封闭所述缺口，在处于第二位置时暴露所述缺口；以及用于推动翻板翻转的推动装置（50）。该登机桥接机口装置安装在登机桥的接机平台的前端，可同时服务左右开门的飞机及下翻开门的飞机。还公开了一种具有该登机桥接机口装置的登机桥及其接机方法。

Description

一种登机桥接机口装置和具有其的登机桥及其接机方法
技术领域
本发明涉及一种登机桥，尤其涉及一种登机桥接机口装置和具有该装置的 登机桥及其接机方法。
登机桥作为连接候机楼与飞机的桥梁，为进出机场的旅客提供安全舒适的 行走空间，在机场已得到广泛的使用。 目前大部分的登机桥可以为左右开门的 飞机进行对接服务，但现有的支线飞机，其飞机机门设计为下翻开带舷梯扶手 的形式， 即为下翻开门的飞机， 因此在一些支线飞机较多的国家和地区， 现有 的为左右开门的飞机设计的登机桥接机口，服务于下翻开门的飞机机门时会发 生干涉， 无法服务此种飞机， 不能符合支线飞机与登机桥之间的对接要求。 发明公开
本发明所要解决的技术问题是提供一种登机桥接机口装置和具有该装置 的登机桥及其接机方法， 可同时服务左右开门的飞机及下翻开门的飞机。
为了实现上述目的， 本发明提供了一种登机桥接机口装置， 安装在登机桥 的接机平台的前端， 其包括：
活动地板主体，所述活动地板主体的后端与所述接机平台的前端连接，所 述活动地板主体的前端设置有一缺口，所述缺口适于容纳一飞机的机门下翻或 上翻；
翻板，对应于该缺口设置并与所述活动地板主体活动连接， 且所述翻板相 对于所述活动地板主体在一第一位置与一第二位置之间翻转，所述翻板在处于 所述第一位置时封闭所述缺口， 在处于所述第二位置时暴露所述缺口； 以及 推动装置， 用于推动所述翻板翻转， 所述推动装置包括： 安装支架， 固定 连接在所述活动地板主体的底部； 推进器， 该推进器的一端连接在所述安装支 架上， 该推进器的另一端连接在所述翻板的底部。
上述的登机桥接机口装置， 其中，所述的登机桥接机口装置还包括有半自 动锁销机构， 其包括： 锁舌安装结构， 设置于所述翻板底部， 所述锁舌安装结 构上安装有锁舌， 所述锁舌上套装有第一弹簧； 第一锁孔安装结构， 对应于所 述翻板处于所述第一位置时所述锁舌安装结构的位置而对应设置于所述活动 地板主体底部的第一安装位置上，所述第一锁孔安装结构上具有用于容纳所述 锁舌的第一锁孔； 其中， 所述锁舌的拔出为人工操作， 所述锁舌的复位通过所 述弹簧自动复位，且所述翻板在处于所述第一位置时通过所述锁舌容纳于所述 第一锁孔内而与所述活动地板主体锁紧连接。
上述的登机桥接机口装置， 其中， 所述半自动锁销机构还包括： 第二锁孔 安装结构，对应于所述翻板处于所述第二位置时所述锁舌安装结构的位置而对 应设置于所述活动地板主体底部的第二安装位置上，所述第二锁孔安装结构上 具有用于容纳所述锁舌的第二锁孔； 其中，所述翻板在处于所述第二位置时通 过所述锁舌容纳于所述第二锁孔内而与所述活动地板主体锁紧连接。
上述的登机桥接机口装置，其中，所述半自动锁销机构还包括：感应开关， 对应于所述第一锁孔和所述第二锁孔设置于所述第一锁孔安装结构和所述第 二锁孔安装结构上； 垫板， 对应设置于所述第一锁孔和所述第二锁孔内。
上述的登机桥接机口装置， 其中， 所述半自动锁销机构还包括： 挡片， 对 应于所述第一锁孔和所述第二锁孔活动安装于所述活动地板主体上。
上述的登机桥接机口装置， 其中，所述半自动锁销机构对称设置于所述翻 板前端底部的左右两侧。
上述的登机桥接机口装置， 其中，所述翻板的左右两侧面的至少一侧面上 还分别设置有梯形导向块， 所述梯形导向块的两个梯形斜面为上下布置。
上述的登机桥接机口装置， 其中，在对应于所述翻板的左右两侧的至少一 侧的所述活动地板主体的底部上还设置有压力传感装置，每一所述压力传感装 置包括： 杠杆机构， 其包括弯杆、 直杆、 楔块和第二弹簧， 其中所述弯杆的一 端铰接在所述活动地板主体的底部， 另一端与所述直杆铰接； 所述第二弹簧的 一端连接到所述活动地板主体的底部， 另一端连接到所述弯杆上； 所述楔块固 定连接在所述弯杆的所述一端上； 滑动机构， 其包括滑槽和滑块， 所述滑槽固 定安装在所述活动地板主体的底部，所述滑块固定安装在所述直杆上； 压力传 感器， 固定安装在所述直杆上。
上述的登机桥接机口装置， 其中， 所述弯杆包括第一部分、第二部分和第 三部分， 其中所述第三部分为弯折部分，且所述第三部分的两端分别为所述弯 杆与所述活动地板主体的底部铰接的第一铰接点及所述弯杆与所述直杆铰接 的第二铰接点，所述第一部分与所述第三部分连接于所述第一铰接点， 且所述 楔块固定连接于所述第一部分上，所述第二部分连接于所述第一部分和所述第 三部分之间。
上述的登机桥接机口装置， 其中，所述第二弹簧的另一端的连接位置靠近 于所述第二铰接点。
上述的登机桥接机口装置， 其中，所述活动地板主体的前端和所述翻板的 前端上设置有可拆卸的前缘。
上述的登机桥接机口装置， 其中，所述的登机桥接机口装置还包括一可搬 运的活动渡板，所述可搬运的活动渡板用以在所述翻板处于所述第二位置时封 闭所述缺口。
为了更好地实现上述目的， 本发明还提供了一种登机桥，所述登机桥包括 有接机平台， 其中，所述登机桥还包括连接在所述接机平台前端的如上所述的 登机桥接机口装置。
为了更好地实现上述目的，本发明还提供了一种利用如上所述的登机桥的 接机方法， 其中， 包括：
在服务左右开门的飞机时， 将登机桥接机口装置的翻板上翻到第一位置， 使所述翻板封闭所述登机桥接机口装置的活动地板主体上的缺口，形成一个完 整的接机通道，并操作所述登机桥使所述登机桥接机口装置与该左右开门的飞 机的机门搭接形成一接机通道进行接机 ·'
在服务下翻开门的飞机时， 先将接机口装置的翻板下翻到第二位置， 以暴 露出所述登机桥接机口装置的活动地板主体上的缺口，然后将暴露出的所述缺 口对准该下翻开门的飞机的机门， 并操作登机桥使所述缺口完全容纳所述机 门，接着利用可搬运的活动渡板的一端搭接在所述登机桥接机口装置上并封闭 所述缺口， 另一端搭接在该飞机的地板面上， 形成一接机通道进行接机。
以下结合附图和具体实施例对本实用新型进行详细描述，但不作为对本实 用新型的限定。 附图简要说明
图 1为根据本发明一实施方式的登机桥接机口装置的侧面示意图， 其中示 出了翻板处于第一位置 A和向第二位置 A' 翻转时的两种不同状态，且所述登机 桥接机口装置处于未接机状态；
图 2为图 1所示的登机桥接机口装置的俯视示意图 （翻板处于第一位置 A ) ;
- Π的剖视示意图；
Figure imgf000006_0001
图 5为沿图 3中 13- 13的剖视示意图；
图 6为图 2的登机桥接机口装置的主视示意图；
图 7为图 6中 C部分结构的放大示意图；
图 8为沿图 6中 14- 14的剖视示意图；
图 9为沿图 2中 15- 15的剖视示意图， 其中示出了翻板处于第一位置 A时的 侧面示意图；
图 10为相对于图 9的翻板处于第二位置 A' 时的侧面示意图；
图 11为飞机机门打开时的示意图；
图 12为根据本发明一实施方式的登机桥接机口装置的侧面示意图，其中所 述登机桥接口装置处于接机状态。
下面结合附图对本发明的结构原理和工作原理作具体的描述：
如图 1示出了根据本发明的一实施方式的登机桥 100， 其包括有接机平台 10和登机桥接机口装置 20。其中所述登机桥接机口装置 20安装在所述接机平 台 10的前端， 用于与飞机机门进行对接。
结合参考图 2， 本发明的登机桥接机口装置 20包括有活动地板主体 30和 翻板 40以及推动装置 50。 其中， 所述活动地板主体 30后端 B的左右两侧上 设有渡板 321、 322 , 可选地， 所述渡板 321、 322为三角形结构， 用于与接机 平台 10 (图 2中未示出）连接。 所述活动地板主体 30的前端 F上设置有一缺 口 31 (图 2中缺口 31被翻板 40挡住）， 所述缺口 31可适于容纳一飞机的机 门下翻或上翻。 优选地， 该缺口 31为方型。 所述翻板 40对应于所述缺口 31 设置， 并与所述活动地板主体 30活动连接， 例如通过翻板铰链 41在所述缺口 31后端边上与所述活动地板主体 30铰接， 从而使所述翻板 40可沿着翻板铰 链 41相对于活动地板主体 30进行一定角度的翻转，如图 1中即示出了所述翻 板 40处于第一位置 A时封闭所述缺口 31的状态（双点划线所示）及所述翻板 40向第二位置 A' 翻转时的状态。 所述翻板 40翻转到第二位置 A' 的侧面示 意图如图 10所示， 此时所述缺口 31露出， 以便于具有下翻开门的飞机的机门 下翻。所述第一位置 A为翻板 40与活动地板主体 30相平时的位置， 即所述接 机口装置 20服务于左右开门的飞机时的工作位置； 所述第二位置 A' 为翻板 40与活动地板主体 30之间的角度大于 90 ° 的某一位置 （根据需要确定）， 即 所述接机口装置 20服务于下翻开门的飞机时的工作位置。 其中， 推动装置 50 用于推动所述翻板 40翻转。 可选地， 该推动装置 50包括安装支架 51和推进 器 52， 其中， 安装支架 51固定连接在活动地板主体 30的底部， 推进器 52的 一端连接（可选地， 通过销轴连接）在安装支架 51上， 推进器 52的另一端连 接（可选地， 通过销轴连接）在翻板 40的底部。 较佳地， 所述推进器 52大致 沿所述翻板 40的中线布置， 其另一端连接于所述翻板 40底部的中心位置。
较佳地， 在所述活动地板主体 30的前端（缺口 31以外的前端）设置有可 拆卸前缘 331、 332、 333， 在所述翻板 40的前端上也对应设置有可拆卸的前 缘 43， 以在对接过程中加强对飞机的保护。 安装后的前缘 331、 332、 333和 43的外边缘基本保持平齐。根据本发明的一具体实施例，可拆卸前缘 331、332、 333和可拆卸前缘 43可通过螺栓和螺母与活动地板主体 30和翻板 40连接（如 图 9、 10所示）， 当前缘损坏需要更换或维修时， 其拆卸过程较为便利。
如图 2所示， 本发明的登机桥接机口装置 20还可包括有半自动锁销机构 37。在本实施例中，所述半自动锁销机构 37是对称设置在所述翻板 40前端底 部的左右两侧。 结合参考图 3-图 5， 所述半自动锁销机构 37包括对应安装的 第一锁孔安装结构 371和锁舌安装结构 372。 其中， 所述锁舌安装结构 372是 设置于所述翻板 40的底部， 并安装有锁舌 374， 所述锁舌 374上套装有第一 弹簧 376。所述第一锁孔安装结构 371则是对应于所述翻板 40处于第一位置 A 时所述锁舌安装结构 372的位置而对应设置于所述活动地板主体 30底部的第 一安装位置上， 例如对应设置于所述活动地板主体 30前端底部上， 且所述第 一锁孔安装结构 371上具有用于容纳所述锁舌 374的第一锁孔 373。在本实施 例中， 为了防止误操作， 以及防止有旅客或工作人员站在接机口时操作翻板 40而发生危险， 本发明采用半自动锁销机构 37， 即所述锁舌 374的拔出为人 工操作，所述锁舌 374的复位则是通过所述第一弹簧 376自动复位。在其它实 施例中， 所述半自动锁销机构 37也可以采用其它锁紧机构锁紧所述翻板， 所 述半自动锁销机构 37也可以仅设置在所述翻板 40前端底部的左侧或右侧上， 这些并不作为对本发明的限制。
结合参考图 9， 所述半自动锁销机构 37还包括： 左右对称设置的两个第 二锁孔安装结构 37 Γ ，其对应于所述翻板 40处于所述第二位置 A' 时所述锁 舌安装结构 372的位置而对应设置于所述活动地板主体 30底部的第二安装位 置上， 每一所述第二锁孔安装结构 37Γ 上具有用于容纳所述锁舌 374的第二 锁孔 373 ' 。 其中， 如图 9所示， 所述翻板 40在处于所述第一位置 A时是通 过由第一锁孔安装结构 371和锁舌安装结构 372组成的锁紧结构 37a而与所述 活动地板主体 30进行锁紧连接， 此时， 所述锁舌 374是容纳于所述第一锁孔 373内， 且所述翻板 40基本与活动地板主体 30相平。 如图 10所示， 所述翻 板 40处于所述第二位置 A' 时是通过由第二锁孔安装结构 37Γ 和锁舌安装结 构 372组成的锁紧结构 37a' 而与所述活动地板主体 30进行锁紧连接， 此时， 所述锁舌 374是容纳于所述第二锁孔 373 ' 内， 且所述翻板 40处于所述第二 位置 A' 时， 飞机机门下翻时不会与翻板 40发生干涉。
继续参考图 3， 较佳地， 在所述第一锁孔安装结构 371上还设置有感应开 关 375和垫板 377。其中，所述感应开关 375是对应于所述第一锁孔 373设置， 用以检测锁舌 374是否复位到预定位置；所述垫板 377对应设置于所述第一锁 孔 373内， 用以防止锁舌 374碰触损坏感应开关 375， 以及使得锁舌 374复位 后与感应开关 375的距离达到预定值。相应地，在所述第二锁孔安装结构 37Γ 上也可设置有感应开关和垫板， 其结构、作用和设置位置与图 3所示的感应开 关 375、 垫板 377相类似， 即位于所述第二锁孔安装结构 37Γ 上的感应开关 是对应于所述第二锁孔 373 ' 设置， 位于所述第二锁孔安装结构 37 Γ 上的垫 板是对应设置于所述第二锁孔 373 ' 内。
如图 4所示， 并结合参考图 9、 图 10， 较佳地， 所述半自动锁销机构还包 括 4个挡片：对应于两个所述第一锁孔 373活动安装于所述活动地板主体上的 两个挡片 38和对应于两个所述第二锁孔 373 ' 活动安装于所述活动地板主体 上的两个挡片 38 ' 。 较佳地， 所述挡片 38、 38 ' 是通过销轴 381、 38Γ 连接 在活动地板主体上， 且分别设置在所述翻板处于第一位置 A和第二位置 A' 时 的对应位置， 用于人工拔出锁舌 374 后挡住所述第一锁孔 373 和第二锁孔 373 ' 。 更佳地， 在所述活动地板主体 30上对应于所述挡板 38、 38 ' 的上下 两侧的位置上分别设置有上限位件 391、 39Γ 和下限位件 392、 392 ' ， 用于 所述挡板 38、 38 ' 上下转动的限位， 例如：
当需要接下翻开门飞机时， 人工操作从第一锁孔 373拔出锁舌 374后，挡 板 38即在重力矩作用下绕销轴 381向下转动至受所述下限位件 392限位时的 状态， 如图 4中双点划线绘示的挡板 38的状态， 此时挡板 38挡住所述第一锁 孔 373 ;待人工操作按钮后，翻板 40开始由所述第一位置 A向所述第二位置 A ' 翻转， 当翻板 40翻转至最低位置（即翻转至翻板 40重心最低的位置）后， 继 续向上翻转至接近第二锁孔 373 ' 的位置时，锁舌 374向上碰触挤压挡板 38 ' ， 使挡板 38 ' 绕销轴 38 Γ 向上转动至受所述上限位件 39Γ 限位时的状态， 此 时锁舌 374容纳于第二锁孔 373 ' 并锁紧。
当接下翻开门飞机的任务完成后， 由人工操作从第二锁孔 373 ' 拔出锁舌 374后， 挡板 38 ' 即在重力矩作用下绕销轴 38 Γ 向下转动至受所述下限位件 392 ' 限位时的状态， 此时挡板 38 ' 挡住所述第二锁孔 373 ' ； 待人工操作按 钮后， 翻板 40开始由所述第二位置 A' 向所述第一位置 A翻转， 当翻板 40下 翻至最低位置 （即翻转至翻板 40重心最低的位置） 后， 继续向上翻转至接近 第一锁孔 373的位置时，锁舌 374向上碰触挤压挡板 38，使挡板 38绕销轴 381 向上转动至受所述上限位件 391限位时的状态， 如图 4中实线绘示的挡板 38 的状态， 此时锁舌 374容纳于第一锁孔 373并锁紧。
如图 5所示， 较佳地， 在所述翻板 40的左右两侧面上还分别设置有梯形 导向块 36， 其可通过螺钉固定， 并优选为尼龙材质。 所述梯形导向块 36的两 个梯形斜面 361、 362为上下布置， 在翻板 40向第一位置 A和第二位置 A' 翻 转的过程中起导向作用。 梯形导向 36还可使得翻板 40与活动地板主体 30之 间保持一定间距， 防止二者发生干涉或摩擦。在其它实施例中， 所述梯形导向 块 36也可以仅设置在所述翻板 40的左侧面或右侧面上，这些并不作为对本发 明的限制。
如图 6-图 8所示，在靠近所述翻板 40的左右两侧的所述活动地板主体 30 的底部的左右两侧还各设置有一个压力传感装置 60。 在本发明中， 每一所述 压力传感装置 60包括杠杆机构 61、 滑动机构 62和压力传感器 63。
其中， 杠杆机构 61包括弯杆 611、 直杆 612、 楔块 613和第二弹簧 614。 所述弯杆 611的一端通过销轴铰接在所述活动地板主体 30的底部， 另一端与 所述直杆 612通过销轴铰接。所述第二弹簧 614的一端连接到所述活动地板主 体 30的底部， 另一端连接到所述弯杆 611上。 较佳地， 所述弯杆 611包括第 一部分 6111、 第二部分 6112和第三部分 61 13， 其中所述第三部分 6113为弯 折部分， 且所述第三部分 6113的两端分别为所述弯杆 611与所述活动地板主 体 30的底部铰接的第一铰接点 61a及所述弯杆 611与所述直杆 612铰接的第 二铰接点 61b， 所述第一部分 6111与所述第三部分 6113连接于所述第一铰接 点 61a， 且所述楔块 613通过螺钉固定连接在所述弯杆 611的所述一端上， 具 体地说是固定于所述第一部分 61 11上，所述第二部分 6112连接于所述第一部 分 6111和所述第三部分 6113之间。所述第二弹簧 614的所述另一端的连接位 置 61c靠近于所述第二铰接点 61b。
其中， 所述滑动机构 62包括滑槽 621和滑块 622。 所述滑槽 621固定安 装在所述活动地板主体 30的底部，所述滑块 622固定安装在所述直杆 612上。 而所述压力传感器 63是固定安装在所述直杆 612上。
其中，所述压力传感装置 60的工作过程描述如下： 当翻板 40翻转至接近 所述第二位置 A' 的一定位置时，翻板 40与楔块 613发生挤压， 推动弯杆 61 1 绕第一铰接点 61a点转动，从而推动与直杆 612固定连接在一起的左右两个压 力传感器 63在滑动机构 62的配合下沿着垂直于自身的方向滑出（在此过程中 第二弹簧 614被拉伸）。 压力传感器 63的作用是防止接机过程中， 缺口 31两 侧与飞机机门 /悬梯 /悬梯扶手发生干涉或碰撞。
如图 9所示， 其示出了翻板 40处于第一位置 A时的状态， 此时， 翻板 40 与活动地板主体 30相平，此时对应于两个第二锁孔 373， 位置的两个挡片 38， 挡住两个第二锁孔 373 ' 。
如图 10所示， 其示出了翻板 40处于第二位置 A' 时的状态， 此时， 翻板 40与活动地板主体 30成一预定角度， 此时对应于两个第一锁孔 373位置的两 个挡片 38挡住两个第一锁孔 373。
图 1 1为下翻开门的飞机的机门打开时的示意图，此时飞机 90的带有悬梯 扶手 911的机门 91下翻， 暴露出机门门口 92。
图 12为根据本发明一实施方式的登机桥接机口装置处于接机状态时的侧 面示意图， 此时翻板 40处于第二位置 A' ， 且登机桥接机口装置 20通过其活 动地板主体 30上的缺口 31容纳所述机门 91于其中。 并且， 本发明的登机桥 接机口装置 20另配有一个可以搬运的活动渡板（图中未示出）， 用以在所述翻 板 40处于所述第二位置 A' 时封闭缺口 31， 从而形成一个接机通道， 旅客即 可上下飞机。
下面将结合本发明的一实施方式详细说明利用包含本发明登机桥接机口 装置 20的登机桥 100的接机方法：
1 ) 在服务左右开门的飞机时， 将登机桥接机口装置 20的翻板 40翻转至 第一位置 A, 使所述翻板 40封闭所述登机桥接机口装置的活动地板主体 30上 的缺口 31， 并利用半自动锁销机构 37将翻板 40与所述活动地板主体 30牢靠 的锁在一起， 从而形成一个完整的接机通道， 然后操作登机桥使所述登机桥接 机口装置 20与该左右开门的飞机的机门搭接形成一接机通道进行接机， 此时 同普通的接机口一样可以服务左右开门的飞机。
2 )当需要服务下翻开门的飞机时， 操作人员可先到接机平台 10下方， 将 半自动锁销机构 37的锁舌拔出 （考虑人工拔锁舌的原因在于防止操作人员误 操作，若有工作人员或旅客站在接机平台上操作员如误操作翻板下翻则会危及 人员生命， 故此处需要操作人员人工拔锁舌）； 拔出锁舌后， 操作人员上到登 机桥上， 按动按钮使翻板 40翻转， 当翻板 40翻转至接近所述第二位置 A' 的 一定位置时，翻板 40与杠杆机构 61的楔块 613发生挤压，将安装在杠杆机构 61上的压力传感器 63通过滑动机构 62滑出到翻板翻开的缺口 31的两侧（压 力传感器翻出后，在接机时可以检测飞机机门 /舷梯 /悬梯扶手是否将碰到缺口 周围的结构）； 翻板 40继续翻转至第二位置 A ' 时， 半自动锁销机构 37的锁 舌自动弹入对应的锁孔并锁紧； 操作人员将翻板 40翻出的缺口 31对准机门 91，操作登机桥前进直至接机口装置 20接触到机身，此时缺口 31完全容纳了 机门 91 ; 然后操作人员将可搬运的活动渡板的一端搭在登机桥接机口装置 20 上并封闭缺口 31， 另一端搭在飞机地板面上， 形成一个接机通道， 旅客即可 上下飞机。
接机结束后， 操作人员将可搬运的活动渡板收回； 退桥直到将机门 91完 全退出缺口 31外；然后下到接机平台下方将锁住的半自动锁销机构 37的锁舌 374拔出， 并按动按钮使翻板 40由第二位置 A' 向第一位置 A翻转，在此过程 中， 翻板 40逐渐不再挤压杠杆机构 61， 压力传感器 63在第二弹簧 614的作 用下收回； 翻板 40继续上翻到位时， 半自动锁销机构 37的锁舌自动弹入对应 的锁孔并锁紧， 此时翻板 40处于第一位置 A, 接机过程完毕。
当然， 本发明还可有其它多种实施例，在不背离本发明精神及其实质的情 况下， 熟悉本领域的技术人员当可根据本发明作出各种相应的改变和变形，但 这些相应的改变和变形都应属于本发明所附的权利要求的保护范围。 工业应用性
利用本发明的登机桥接机口装置和具有其的登机桥，可同时服务左右开门 的飞机及下翻开门的飞机， 可以很好地满足支线飞机与登机桥之间的对接要 求。

Claims

权利要求书
1、 一种登机桥接机口装置， 安装在登机桥的接机平台的前端， 其特征在 于， 包括有：
活动地板主体，所述活动地板主体的后端与所述接机平台的前端连接，所 述活动地板主体的前端设置有一缺口，所述缺口适于容纳一飞机的机门下翻或 上翻；
翻板，对应于该缺口设置并与所述活动地板主体活动连接， 且所述翻板相 对于所述活动地板主体于在一第一位置与一第二位置之间翻转，所述翻板在处 于所述第一位置时封闭所述缺口，在处于所述第二位置时暴露所述缺口； 以及 推动装置， 用于推动所述翻板翻转， 所述推动装置包括：
安装支架， 固定连接在所述活动地板主体的底部；
推进器， 该推进器的一端连接在所述安装支架上， 该推进器的另一端 连接在所述翻板的底部。
2、 根据权利要求 1所述的登机桥接机口装置， 其特征在于， 还包括有半 自动锁销机构， 其包括：
锁舌安装结构， 设置于所述翻板底部， 所述锁舌安装结构上安装有锁舌， 所述锁舌上套装有第一弹簧；
第一锁孔安装结构，对应于所述翻板处于所述第一位置时所述锁舌安装结 构的位置而对应设置于所述活动地板主体底部的第一安装位置上，所述第一锁 孔安装结构上具有用于容纳所述锁舌的第一锁孔；
其中，所述锁舌的拔出为人工操作， 所述锁舌的复位通过所述弹簧自动复 位，且所述翻板在处于所述第一位置时通过所述锁舌容纳于所述第一锁孔内而 与所述活动地板主体锁紧连接。
3、 根据权利要求 2所述的登机桥接机口装置， 其特征在于， 所述半自动 锁销机构还包括：
第二锁孔安装结构，对应于所述翻板处于所述第二位置时所述锁舌安装结 构的位置而对应设置于所述活动地板主体底部的第二安装位置上，所述第二锁 孔安装结构上具有用于容纳所述锁舌的第二锁孔；
其中，所述翻板在处于所述第二位置时通过所述锁舌容纳于所述第二锁孔 内而与所述活动地板主体锁紧连接。
4、 根据权利要求 3所述的登机桥接机口装置， 其特征在于， 所述半自动 锁销机构还包括：
感应开关，对应于所述第一锁孔和所述第二锁孔设置于所述第一锁孔安装 结构和所述第二锁孔安装结构上；
垫板， 对应设置于所述第一锁孔和所述第二锁孔内。
5、 根据权利要求 4所述的登机桥接机口装置， 其特征在于， 所述半自动 锁销机构还包括：
挡片，对应于所述第一锁孔和所述第二锁孔活动安装于所述活动地板主体 上。
6、 根据权利要求 3所述的登机桥接机口装置， 其特征在于， 所述半自动 锁销机构对称设置于所述翻板前端底部的左右两侧。
7、 根据权利要求 3所述的登机桥接机口装置， 其特征在于， 所述翻板的 左右两侧面的至少一侧面上还设置有梯形导向块，所述梯形导向块的两个梯形 斜面为上下布置。
8、 根据权利要求 3所述的登机桥接机口装置， 其特征在于， 在对应于所 述翻板的左右两侧的至少一侧的所述活动地板主体的底部上还设置有压力传 感装置， 所述压力传感装置包括：
杠杆机构， 其包括弯杆、 直杆、 楔块和第二弹簧， 其中所述弯杆的一端铰 接在所述活动地板主体的底部， 另一端与所述直杆铰接； 所述第二弹簧的一端 连接到所述活动地板主体的底部， 另一端连接到所述弯杆上； 所述楔块固定连 接在所述弯杆的所述一端上；
滑动机构， 其包括滑槽和滑块，所述滑槽固定安装在所述活动地板主体的 底部， 所述滑块固定安装在所述直杆上；
压力传感器， 固定安装在所述直杆上。
9、 根据权利要求 8所述的登机桥接机口装置， 其特征在于， 所述弯杆包 括第一部分、第二部分和第三部分， 其中所述第三部分为弯折部分， 且所述第 三部分的两端分别为所述弯杆与所述活动地板主体的底部铰接的第一铰接点 及所述弯杆与所述直杆铰接的第二铰接点，所述第一部分与所述第三部分连接 于所述第一铰接点， 且所述楔块固定连接于所述第一部分上，所述第二部分连 接于所述第一部分和所述第三部分之间。
10、 根据权利要求 9所述的登机桥接机口装置， 其特征在于， 所述第二弹 簧的另一端的连接位置靠近于所述第二铰接点。
11、 根据权利要求 1所述的登机桥接机口装置， 其特征在于， 所述活动地 板主体的前端和所述翻板的前端上设置有可拆卸的前缘。
12、 根据权利要求 1所述的登机桥接机口装置， 其特征在于， 还包括一可 搬运的活动渡板，所述可搬运的活动渡板用以在所述翻板处于所述第二位置时 封闭所述缺口。
13、 一种登机桥， 所述登机桥包括有接机平台， 其特征在于， 所述登机桥 还包括连接在所述接机平台前端的如权利要求 1-12中任意一项所述的登机桥 接机口装置。
14、 一种利用如权利要求 13所述的登机桥的接机方法， 其特征在于， 包 括：
在服务左右开门的飞机时， 将登机桥接机口装置的翻板上翻到第一位置， 使所述翻板封闭所述登机桥接机口装置的活动地板主体上的缺口，形成一个完 整的接机通道，并操作所述登机桥使所述登机桥接机口装置与该左右开门的飞 机的机门搭接形成一接机通道进行接机；
在服务下翻开门的飞机时， 先将接机口装置的翻板下翻到第二位置， 以暴 露出所述登机桥接机口装置的活动地板主体上的缺口，然后将暴露出的所述缺 口对准该下翻开门的飞机的机门， 并操作登机桥使所述缺口完全容纳所述机 门，接着利用可搬运的活动渡板的一端搭接在所述登机桥接机口装置上并封闭 所述缺口， 另一端搭接在该飞机的地板面上， 形成一接机通道进行接机。
PCT/CN2013/081213 2012-09-17 2013-08-09 一种登机桥接机口装置和具有其的登机桥及其接机方法 WO2014040462A1 (zh)

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EP2896569A4 (en) 2016-01-20
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AU2013314929A1 (en) 2015-05-07
CA2885108C (en) 2017-06-13
US9434482B2 (en) 2016-09-06
US20150274324A1 (en) 2015-10-01
CA2885108A1 (en) 2014-03-20
BR112015005805A2 (pt) 2017-07-04
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EP2896569A1 (en) 2015-07-22
CN103662074A (zh) 2014-03-26

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